An aircraft fuel tank inerting system is disclosed. An aircraft fuel tank inerting system may include a paramagnetic pump arranged to apply a magnetic field to a source of gas to provide a motivational force for removing oxygen from said gas. A paramagnetic pump may include a series of magnetic field generating elements configured to provide a sequence of discrete spaced apart magnetic fields. The series of magnetic field generating elements may include a series of spaced apart pairs of magnetic field generating elements. Each spaced apart pair of magnetic field generating elements may be arranged to generate a respective spaced apart magnetic field, of the sequence of discrete spaced apart magnetic fields, across an airspace therebetween.


    Access

    Download


    Export, share and cite



    Title :

    FUEL TANK INERTING


    Contributors:

    Publication date :

    2018-11-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    FUEL TANK INERTING

    PANKAJ SHIREESH / JOSHI MAHESH PRABHAKAR / GUPTA SWARNIM et al. | European Patent Office | 2017

    Free access

    FUEL TANK INERTING

    PANKAJ SHIREESH / GUPTA SWARNIM / JOSHI MAHESH PRABHAKAR et al. | European Patent Office | 2017

    Free access

    FUEL TANK INERTING SYSTEM AND METHOD FOR FUEL TANK INERTING

    RHEAUME JONATHAN / PERRY MICHAEL L | European Patent Office | 2021

    Free access

    FUEL TANK INERTING

    PANKAJ SHIREESH / JOSHI MAHESH PRABHAKAR / GUPTA SWARNIM et al. | European Patent Office | 2020

    Free access

    Fuel tank inerting

    PANKAJ SHIREESH / JOSHI MAHESH PRABHAKAR / GUPTA SWARNIM et al. | European Patent Office | 2021

    Free access